AD 2013-21-05R1
final rule
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | Airbus Helicopters Deutschland GmbH | EC135P1 | Airworthiness Directives; Airbus Helicopters Deutschland GmbH (Previously Eurocopter Deutschland GmbH) Helicopters |
| aircraft | Airbus Helicopters Deutschland GmbH | EC135P2 | Airworthiness Directives; Airbus Helicopters Deutschland GmbH (Previously Eurocopter Deutschland GmbH) Helicopters |
| aircraft | Airbus Helicopters Deutschland GmbH | EC135P2+ | Airworthiness Directives; Airbus Helicopters Deutschland GmbH (Previously Eurocopter Deutschland GmbH) Helicopters |
| aircraft | Airbus Helicopters Deutschland GmbH | EC135T1 | Airworthiness Directives; Airbus Helicopters Deutschland GmbH (Previously Eurocopter Deutschland GmbH) Helicopters |
| aircraft | Airbus Helicopters Deutschland GmbH | EC135T2 | Airworthiness Directives; Airbus Helicopters Deutschland GmbH (Previously Eurocopter Deutschland GmbH) Helicopters |
| aircraft | Airbus Helicopters Deutschland GmbH | EC135T2+/EC635T2+ | Airworthiness Directives; Airbus Helicopters Deutschland GmbH (Previously Eurocopter Deutschland GmbH) Helicopters |
Unsafe Condition
Tail Rotor Control System
Source: Official FAA Source ↗
Retrieved: Apr 8, 2026
Rights: U.S. Government Public Domain
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